View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 06173U 26053.17937625 +.00000000 +00000-0 +14640-3 0 00004
2 06173 90.0135 208.4623 0051924 70.8222 106.4485 14.52513331 00
| Epoch (UTC): | 22 February 2026 04:18:18 |
| Eccentricity: | 0.0051924 |
| inclination: | 90.0135° |
| perigee height: | 681 km |
| apogee height: | 754 km |
| right ascension of ascending node: | 208.4623° |
| argument of perigee: | 70.8222° |
| revolutions per day: | 14.52513331 |
| mean anomaly at epoch: | 106.4485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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